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Little Wing Autogyro
from Wikipedia

The Little Wing Autogyro is a series of conventional one and two place autogyros with a tractor engine layout using modern engines and produced by Little Wing Autogyros, Inc. of Mayflower, Arkansas.[1][2][3][4]

Key Information

Development

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Ron Herron was concerned about the problem of pushover fatalities in pusher gyrocopters. He set to develop a tractor layout gyrocopter that also met the FAA rules for ultralight aircraft. A Prototype LW-1 powered by a Continental O-200 engine was soon followed on by the LW-2. The design was influenced by Juan de la Cierva's autogyros. [5]

Operational history

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Andy Keech set 29 world records in an LW-5 Autogyro.[6][7][8][9][10][11][12]

Variants

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LW-1
Original proof of concept prototype
LW-2
Single place autogyro designed to weigh less than 254 lb (115 kg) to meet US FAR 103 Ultralight Vehicles regulations
LW-3
A 70 hp (52 kW) covered version
LW-4
A two place long frame version
LW-5
A two place short frame version
Roto-Pup
Ultralight version based on the Preceptor Ultra Pup airframe.[1][13]

Aircraft on display

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Specifications (LW-2)

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Data from Company[15]

General characteristics

  • Crew: 1
  • Length: 18 ft (5.5 m)
  • Height: 8 ft 5 in (2.57 m)
  • Gross weight: 750 lb (340 kg)
  • Fuel capacity: 8.5 U.S. gallons (32 L; 7.1 imp gal)
  • Main rotor diameter: 23 ft (7.0 m)
  • Main rotor area: 415 sq ft (38.6 m2)
  • Propellers: 2-bladed

Performance

  • Cruise speed: 65 kn (75 mph, 121 km/h)
  • Disk loading: 1.8 lb/sq ft (8.8 kg/m2)

See also

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Aircraft of comparable role, configuration, and era

References

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